System and method for managing residual energy for an electric aircraft

1. A system for managing residual energy for an electric aircraft, wherein the system comprises:

a battery pack incorporated in an electric aircraft, wherein the battery pack comprises:

a plurality of battery modules; and

at least a pack monitor unit, wherein the at least a pack monitor unit is configured to generate a battery pack datum;

at least a battery management system, wherein the battery management system further comprises a plurality of battery management components such that at least one of the plurality of battery management components is operational;

a charging component electrically connected to the battery pack;

a sensor communicatively connected to the charging component, wherein the sensor is configured to:

detect at least an electrical parameter of the charging component and the electric aircraft; and

generate a residual datum as a function of the at least an electrical parameter and the battery pack datum;

a computing device, wherein the computing device is configured to:

receive the residual datum from the sensor;

identify a residual element as a function of the residual datum, wherein the residual element comprises at least a leakage current;

generate a residual prediction datum as a function of the residual element identified;

compare the residual element and the residual prediction;

generate an alert datum as a function of the comparison of the residual element and the residual prediction datum; and

execute a security measure as a function of the alert datum.

2. The system of claim 1 , wherein the electric aircraft further comprises an electric vertical take-off and landing aircraft.

3. The system of claim 1 , wherein the security measure further comprises relaying information about the residual element to a user.

4. The system of claim 1 , wherein the computing device is further configured to determine the residual element using a residual threshold.

5. The system of claim 4 , wherein the security measure is selected based on a magnitude of the residual element.

6. The system of claim 1 , wherein the security measured is executed as a function of a trip class.

7. The system of claim 1 , wherein the computing device is configured to operate in a first mode, wherein the first mode is configured to execute the security measure on the electric aircraft.

8. The system of claim 7 , wherein the first mode is further configured to terminate one or more connections of a battery component to its neighboring battery components, as a function of the identification of the residual element.

9. The system of claim 1 , wherein the computing device is configured to operate in a second mode, wherein the second mode is configured to execute the security measure on the charging component.

10. The system of claim 9 , wherein the second mode is further configured to trip the charging component in the event the residual element is identified within the charging component based on the trip class.

11. A method for managing residual energy for an electric aircraft, wherein the method comprises:

generating, by at least a pack monitor unit, a battery pack datum from a battery pack of an electric aircraft, wherein the battery pack comprises at least a battery management system using a plurality of battery management components such that at least one of the plurality of battery management components is operational;

detecting, by a sensor communicatively connected to a charging component, at least an electrical parameter as a function of the charging component and the electric aircraft;

generating a residual datum as a function of the at least an electrical parameter and the battery pack datum;

receiving, by a computing device, the residual datum;

identifying a residual element as a function of the residual datum, wherein the residual element comprises at least a leakage current;

generating a residual prediction datum as a function of the residual element identified;

comparing the residual element and the residual prediction;

generating an alert datum as a function of the comparison of the residual element and the residual prediction datum; and

executing a security measure as a function of the alert datum.

12. The method of claim 11 , wherein the electric aircraft further comprises an electric vertical take-off and landing aircraft.

13. The method of claim 11 , wherein the executing the security measure further comprises relaying information about the residual element to a user.

14. The method of claim 11 , wherein the method further determining the residual element using a residual threshold.

15. The method of claim 14 , wherein the security measure is selected based on a magnitude of the residual element.

16. The method of claim 11 , wherein executing the security measure further comprises executing as a function of a trip class.

17. The method of claim 11 , wherein the method further comprises operating in a first mode, wherein the first mode is configured to execute the security measure on the electric aircraft.

18. The method of claim 17 , wherein the method further comprises terminating one or more connections of a battery component to its neighboring battery components, as a function of the identification of the residual element.

19. The method of claim 11 , wherein the method further comprises operating in a second mode, wherein the second mode is configured to execute the security measure on the charging component.

20. The method of claim 19 , wherein the method further comprises tripping the charging component in the event the residual element is identified within the charging component based on the trip class.